Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/109678
PIRA download icon_1.1View/Download Full Text
DC FieldValueLanguage
dc.contributorDepartment of Industrial and Systems Engineering-
dc.creatorWang, W-
dc.creatorYung, KL-
dc.date.accessioned2024-11-08T06:11:14Z-
dc.date.available2024-11-08T06:11:14Z-
dc.identifier.issn1742-6588-
dc.identifier.urihttp://hdl.handle.net/10397/109678-
dc.description2023 The 7th International Conference on Mechanical, Aeronautical and Automotive Engineering (ICMAA 2023) 24-26 February 2023, Onlineen_US
dc.language.isoenen_US
dc.publisherInstitute of Physics Publishing Ltd.en_US
dc.rightsContent from this work may be used under the terms of the Creative Commons Attribution 3.0 licence (http://creativecommons.org/licenses/by/3.0). Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI.en_US
dc.rightsPublished under licence by IOP Publishing Ltden_US
dc.rightsThe following publication Wang, W., & Yung, K. L. (2023). Analysis of a Mechanical Anchoring System for Landing on Asteroids. Journal of Physics: Conference Series, 2542(1), 012017 is available at https://doi.org/10.1088/1742-6596/2542/1/012017.en_US
dc.titleAnalysis of a mechanical anchoring system for landing on asteroidsen_US
dc.typeConference Paperen_US
dc.identifier.volume2542-
dc.identifier.issue1-
dc.identifier.doi10.1088/1742-6596/2542/1/012017-
dcterms.abstractThe landing process to an asteroid is discussed with a Nimble Lander. The miniature harpoons are chosen as the anchoring device to landing to asteroid in the Nimble Lander. The analysis results provide detailed information of the anchoring with harpoon as anchoring device. Many different designs of harpoon have been tested by simulation, the best of three designs of harpoon are analyzed for anchoring to Apophis. Instead of the modelling of the anchor as a rigid cylindrical projectile in penetration models, the deformation of the harpoon is fully considered in the anchoring analysis. The analysis provides ground base a reliable design anchoring system for landing to Asteroids.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationJournal of physics. Conference series, 2023, v. 2542, no. 1, 012017-
dcterms.isPartOfJournal of physics. Conference series-
dcterms.issued2023-
dc.identifier.scopus2-s2.0-85173018270-
dc.relation.conferenceInternational Conference on Mechanical, Aeronautical and Automotive Engineering [ICMAA]-
dc.identifier.eissn1742-6596-
dc.identifier.artn012017-
dc.description.validate202411 bcch-
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_Scopus/WOSen_US
dc.description.fundingSourceSelf-fundeden_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryCCen_US
Appears in Collections:Conference Paper
Files in This Item:
File Description SizeFormat 
Wang_2023_J._Phys.__Conf._Ser._2542_012017.pdf778.45 kBAdobe PDFView/Open
Open Access Information
Status open access
File Version Version of Record
Access
View full-text via PolyU eLinks SFX Query
Show simple item record

Page views

3
Citations as of Nov 17, 2024

Downloads

6
Citations as of Nov 17, 2024

Google ScholarTM

Check

Altmetric


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.